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McDonnell Douglas F-15E Strike Eagle
Category | Air Superiority Fighter Tactical Fighter Aircraft | ||||||||
|---|---|---|---|---|---|---|---|---|---|
Origin | United States (McDonnell Douglas) | ||||||||
First Flight and Production Year | 27 July 1972 (First Flight) 1976 (Entry into Service) | ||||||||
Number Produced | More than 1200 | ||||||||
Engine and Power System | 2 × Pratt & Whitney F100 turbofan engines Variable thrust depending on model | ||||||||
Users | United States Air Force (USAF) Israeli Air Force Japan Air Self-Defense Force Royal Saudi Air Force Republic of Korea Air Force | ||||||||
Dimensions | Length: 19.43 metres Wingspan: 13.05 metres Height: 5.63 metres Wing area: 56.5 m² | ||||||||
Weights | Empty weight: Approximately 12700 kg (varies by model) Maximum takeoff weight: 30845 kg | ||||||||
Performance | Maximum speed: Mach 2.5+ (at high altitude) Cruise speed: Mach 0.9 Service ceiling: 19800 metres (65000 ft) Range: 5550 km (with external fuel tanks) | ||||||||
The McDonnell Douglas F-15 Eagle is a twin-engine tactical fighter aircraft developed in the 1970s and subsequently used by numerous air forces. Designed for air superiority missions, the F-15 is renowned for its high maneuverability and advanced avionics systems.
Douglas F-15 (Pixabay)
Following the Vietnam War, the United States Air Force (USAF) identified a need for a fighter aircraft capable of achieving air superiority, prompting McDonnell Douglas to initiate the F-15 Eagle project. The F-15 made its first flight in 1972 and entered service in 1976. The aircraft’s design is distinguished by its twin-engine configuration providing high thrust and advanced avionics systems.
One of the most notable features of the F-15 is its advanced radar and avionics systems, which enable the aircraft to detect, track, and effectively engage targets at long ranges. The aircraft’s weapons systems include a variety of options such as air-to-air missiles, bombs, and a 20 mm cannon. Different variants of the F-15 have been tailored for specific roles; for example, the F-15E Strike Eagle is equipped with air-to-ground attack capabilities and has emerged as a multirole platform.
The F-15 has been deployed in various conflicts including the Gulf War, the Kosovo War, and the Iraq War. It has been effectively utilized in both air superiority and air-to-ground attack missions and continues to serve in the air forces of many countries.
Douglas F-15E Strike Eagle (Pixabay)
The F-15 Eagle holds a significant place among modern combat aircraft. It played a pivotal role in the evolution of the air superiority concept and became one of the iconic symbols of the Cold War era. The aircraft has inspired the design of numerous subsequent fighter jets.
Douglas F-15 Eagle (Pixabay)
"BilalBulut.net." "F-15 Eagle - BilalBulut.net." Accessed April 15, 2025.http://www.bilalbulut.net/ucak/data.aspx?content=f-15
"F-15 Eagle." Air Force. Fact Sheet Display. AF.mil. Accessed April 15, 2025.
"McDonnell Douglas F-15 Streak Eagle." National Museum of the U.S. Air Force. Accessed April 15, 2025.
Doyle, David. F-15 Eagle: McDonnell Douglas Strike Fighter (Legends of Warfare: Aviation, 62). Atglen, PA: Schiffer Military History, 2017.
SavunmaTR. "F-15EX Advanced Eagle ve Özellikleri Nedir? - SavunmaTR." Accessed June 14, 2024.https://www.savunmatr.com/f-15ex-advanced-eagle-ve-ozellikleri-nedir/
McDonnell Douglas F-15E Strike Eagle
Category | Air Superiority Fighter Tactical Fighter Aircraft | ||||||||
|---|---|---|---|---|---|---|---|---|---|
Origin | United States (McDonnell Douglas) | ||||||||
First Flight and Production Year | 27 July 1972 (First Flight) 1976 (Entry into Service) | ||||||||
Number Produced | More than 1200 | ||||||||
Engine and Power System | 2 × Pratt & Whitney F100 turbofan engines Variable thrust depending on model | ||||||||
Users | United States Air Force (USAF) Israeli Air Force Japan Air Self-Defense Force Royal Saudi Air Force Republic of Korea Air Force | ||||||||
Dimensions | Length: 19.43 metres Wingspan: 13.05 metres Height: 5.63 metres Wing area: 56.5 m² | ||||||||
Weights | Empty weight: Approximately 12700 kg (varies by model) Maximum takeoff weight: 30845 kg | ||||||||
Performance | Maximum speed: Mach 2.5+ (at high altitude) Cruise speed: Mach 0.9 Service ceiling: 19800 metres (65000 ft) Range: 5550 km (with external fuel tanks) | ||||||||
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